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検索結果 17 件

Multidisciplinary analysis of a hypersonic engine [microform] / M.E.M. Stewart ... [et al.] ; prepared for the 11th International Conference on Space Planes and Hypersonic Systems and Technologies ... September 29-October 4, 2002 (NASA/TM ; 2002-211971)

Multidisciplinary analysis of a hypersonic engine [microform] / M.E.M. Stewart ... [et al.] ; prepared for the 11th International Conference on Space Planes and Hypersonic Systems and Technologies ... September 29-October 4, 2002 (NASA/TM ; 2002-211971)
マイクロ図書
2002<YCA-NAS 1.15:2002-211971>
国立国会図書館
  • 件名Hypersonics Fluid dynamics Structural analysis Thermodynamics Supersonic combustion ramjet engines

Recent flight test results of the joint CIAM-NASA Mach 6.5 Scramjet Flight Program [microform] / Alexander S. Roudakov and Vyacheslav L. Semenov, John W. Hicks (NASA/TP ; 1998-206548)

Recent flight test results of the joint CIAM-NASA Mach 6.5 Scramjet Flight Program [microform] / Alexander S. Roudakov and Vyacheslav L. Semenov, John W. Hicks (NASA/TP ; 1998-206548)
マイクロ図書
1998<YCA-NAS 1.60:206548>
国立国会図書館
  • 件名Supersonic combustion ramjet engines Supersonic combustion Missiles Launching Hypersonic...

Computational analysis of the combustion process in an axisymmetric RBCC flowpath [microform] / Christopher J. Steffen, Shaye Yungster ([NASA technical memorandum] ; NASA/TM-2001-210679)

Computational analysis of the combustion process in an axisymmetric RBCC flowpath [microform] / Christopher J. Steffen, Shaye Yungster ([NASA technical memorandum] ; NASA/TM-2001-210679)
マイクロ図書
2001<YCA-NAS 1.15:210679>
国立国会図書館
  • 件名...nsional models Supersonic combustion ramjet engines Simulation

A two-line absorption instrument for scramjet temperature and water vapor concentration measurement in HYPULSE [microform] / C.Y. Tsai ([NASA contractor report] ; NASA/CR-1998-207664)

A two-line absorption instrument for scramjet temperature and water vapor concentration measurement in HYPULSE [microform] / C.Y. Tsai ([NASA contractor report] ; NASA/CR-1998-207664)
マイクロ図書
1998<YCA-NAS 1.26:207664>
国立国会図書館
  • 件名Combustion chambers Supersonic combustion ramjet engines Temperature me...

Hyper-X wind tunnel program [microform] / C.R. McClinton ... [et al.] ([NASA technical memorandum] ; 207317)

Hyper-X wind tunnel program [microform] / C.R. McClinton ... [et al.] ([NASA technical memorandum] ; 207317)
マイクロ図書
1998<YCA-NAS 1.15:207317>
国立国会図書館
  • 件名Supersonic combustion ramjet engines Research vehic...

Development of a flush airdata sensing system on a sharp-nosed vehicle for flight at Mach 3 to 8 [microform] / Mark C. Davis ... [et al.] ([NASA technical memorandum] ; NASA/TM-2000-209017)

Development of a flush airdata sensing system on a sharp-nosed vehicle for flight at Mach 3 to 8 [microform] / Mark C. Davis ... [et al.] ([NASA technical memorandum] ; NASA/TM-2000-209017)
マイクロ図書
2000<YCA-NAS 1.15:209017>
国立国会図書館
  • 件名Mach number Research vehicles Supersonic combustion ramjet engines Wind tunnel te...

Instrumentation development for study of Reynolds analogy in reacting flows [microform] / D.J. DeTurris (NASA technical memorandum ; 110196)

Instrumentation development for study of Reynolds analogy in reacting flows [microform] / D.J. DeTurris (NASA technical memorandum ; 110196)
マイクロ図書
1995<YCA-NAS 1.15:110196>
国立国会図書館
  • 件名...n Strain gages Supersonic combustion Supersonic combustion ramjet engines Supersonic flo...

Shock tunnel studies of scramjet phenomena [microform] : final technical report, NAGW-674 ([NASA contractor report] ; NASA-CR-203578)

Shock tunnel studies of scramjet phenomena [microform] : final technical report, NAGW-674 ([NASA contractor report] ; NASA-CR-203578)
マイクロ図書
1996<YCA-NAS 1.26:203578>
国立国会図書館
  • 件名...py Mach number Supersonic combustion ramjet engines Hypersonic noz...

Options for flight testing rocket-based combined-cycle (RBCC) engines [microform] / J. Olds ([NASA contractor report] ; NASA-CR-201897)

Options for flight testing rocket-based combined-cycle (RBCC) engines [microform] / J. Olds ([NASA contractor report] ; NASA-CR-201897)
マイクロ図書
1996<YCA-NAS 1.26:201897>
国立国会図書館
  • 件名Engine tests Flight tests Supersonic combustion ramjet engines Rocket engines...

Experimental investigation of inlet-combustor isolators for a dual-mode scramjet at a Mach number of 4 [microform] / Saied Enami ... [et al.] (NASA technical paper ; 3502)

Experimental investigation of inlet-combustor isolators for a dual-mode scramjet at a Mach number of 4 [microform] / Saied Enami ... [et al.] (NASA technical paper ; 3502)
マイクロ図書
1995<YCA-NAS 1.60:3502>
国立国会図書館
  • 件名...formance tests Supersonic combustion ramjet engines Supersonic spe...

Parametric studies of the ejector process within a turbine-based combined-cycle propulsion system [microform] / Nicholas J. Georgiadis, James F. Walker, and Charles J. Trefny ([NASA technical memorandum] ; NASA/TM-1999-209172)

Parametric studies of the ejector process within a turbine-based combined-cycle propulsion system [microform] / Nicholas J. Georgiadis, James F. Walker, and Charles J. Trefny ([NASA technical memorandum] ; NASA/TM-1999-209172)
マイクロ図書
1999<YCA-NAS 1.15:209172>
国立国会図書館
  • 件名...configurations Supersonic combustion ramjet engines Two dimensiona...

Internal aerodynamics of a generic three-dimensional scramjet inlet at Mach 10 [microform] / Scott D. Holland (NASA technical paper ; 3476)

Internal aerodynamics of a generic three-dimensional scramjet inlet at Mach 10 [microform] / Scott D. Holland (NASA technical paper ; 3476)
マイクロ図書
1995<YCA-NAS 1.60:3476>
国立国会図書館
  • 件名...ve interaction Supersonic combustion ramjet engines Wind tunnel te...

複合エンジンの研究開発

複合エンジンの研究開発
デジタル文書・図像類
若松, 義男, 鎮西, 信夫, 三谷, 徹, Wakamatsu, Yoshio, Chinzei, Nobuo, Mitani, Toru宇宙航空研究開発機構2004-10-29宇宙航空研究開発機構研究開発資料: 平成15年度総合技術研究本部宇宙領域研究成果報告書:輸送系 = JAXA Research and Development Memorandum: FY15 Annual Report of Research & Development on Space Technology in the Institute of Space Technology and Aeronautics: Space Transportation SystemJAXA-RM-04-009p.27-30
全国の図書館
  • 件名...d-cycle engine supersonic combustion ramjet engine engine test wal...

飛行マッハ数6条件におけるスクラムジェットエンジンモデルの試験

飛行マッハ数6条件におけるスクラムジェットエンジンモデルの試験
デジタル文書・図像類
苅田, 丈士, 斎藤, 俊仁, 工藤, 賢司, 小室, 智幸, 小野, 文衛, Kanda, Takeshi, Saito, Toshihito, Kudo, Kenji, Komuro, Tomoyuki, Ono, Fumiei航空宇宙技術研究所1998-07航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory1364p.1-20
全国の図書館
  • 件名...st Mach number supersonic combustion supersonic flow short strut f...

バロクリニクトルク利用の混合促進

バロクリニクトルク利用の混合促進
デジタル文書・図像類
小幡, 茂男, Obata, Shigeo航空宇宙技術研究所2000-12航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory46p.313-318
全国の図書館
  • 件名...ng enhancement supersonic combustion ramjet numerical analysis Nav...
  • 一般注記...w model of the Supersonic Combustion Ramjet (SCRAM) engine combust...

Mach 6 testing of a scramjet engine model

Mach 6 testing of a scramjet engine model
デジタル文書・図像類
苅田, 丈士, 斎藤, 俊仁, 工藤, 賢司, 小室, 智幸, 小野, 文衛, Kanda, Takeshi, Saito, Toshihito, Kudo, Kenji, Komuro, Tomoyuki, Ono, Fumiei航空宇宙技術研究所1998-02航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory1345Tp.1-22
全国の図書館
  • 件名...facility strut supersonic combustion supersonic flow combustion ef...

矩形断面スクラムジェット燃焼器の実験　2:噴射部形状の影響

矩形断面スクラムジェット燃焼器の実験　2:噴射部形状の影響
デジタル文書・図像類
村上, 淳郎, 小室, 智幸, 工藤, 賢司, Murakami, Atsuo, Komuro, Tomoyuki, Kudo, kenji航空宇宙技術研究所1993-12航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory1220p.1-25
全国の図書館
  • 件名...combution test supersonic combustion mixing efficiency combustion ...

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